A jet engine receives a flow of 150 m/s air at 75 kPa, 5C across an area

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A jet engine receives a flow of 150 m/s air at 75 kPa, 5°C across an area of 0.6 m2 with an exit flow at 450 m/s, 75 kPa, 600 K. Find the mass flow rate and thrust.
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Fundamentals of Thermodynamics

ISBN: 978-0471152323

6th edition

Authors: Richard E. Sonntag, Claus Borgnakke, Gordon J. Van Wylen

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